Method for calculating section torsional rigidity of large-opening structure of double-bubble fuselage

The invention belongs to the field of aviation structure design, and particularly relates to a double-bubble fuselage large-opening structure section torsional rigidity calculation method. Comprising the following steps: constructing a double-bubble fuselage large-opening structure analysis model; c...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: DU PENGLIANG, FENG YAJUN, HUANG YE
Format: Patent
Sprache:chi ; eng
Schlagworte:
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